SCIENTIFIC ABSTRACT YAMPOLSKIY, P. A. - YAMPOLSKIY, V. G.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001962030001-9
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: September 17, 2001
• Sequence Number: 1
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

22126
3/056/61/040/003/006/031
Study of the reactions ... B102/B202
V
the reaction B12O9 (n,2n)Bi2O8m* It was found that the energies of gamma
radiation-accompanying Bi 208m decay were 0#88+0s02 Mev and 0.50+0.02 Mev,
the half-life was 2#6 + 0.1 msec, the reaction oross,section was
0.66 + 0.12 b. Further experiments were made in order to determine the
cross section of reactions which led to the formation of a long-lived nio-
bium isomer as well as experiments for*a more accurate measurement of the
Na 24m half-life. 10-0 + 0*3 d was obtained for the half-life of the isomer
92g
fib i Oe94 + 0-1 Mev for the energy of gamma radiation accompanying its
beta decay. ;he reaction cross section Nb93(np2n)Nbg2a was found to be
61 0-56 + m6 be The sodium isomer was produced in the reaction
92; _24m- 24m
Al (n,,ok)Na 1 the Na life time was found to be 18.3 + 0.6 msec. The
T88M production cross section was d 1:;00-4 be Further ore, the authors
m
calculated the cross section of lead-isomer production assuming that this
Card'2/4

22126
3
Y'0/040/003/006/031
/059B2
Study of the reactions as# B102 02
206 207M
isomer is produced only In the reaction P:b .(p,2n)Pb The value ob-
tained was compared with the one calculated from the strong-interaction
theory by as3uming a two-stage mechanism of neutron-evapo,ration in the
(n,2n) reaction, in this case syb207 level scheme was used which was in
agreement with the shell models p1/2 (ground otate)l ..f,/21,,0-570 Mev;
1'4'633 MOV
P3/2 04894 Mev) 113/2 (metaIS~able4 st'ate)" f7/2- 2;434~Mevl
99/2 2-75 Mev; 111/2 3.60 Mev; d: 5/2 4_42 Mev; g7/2 4e66 MOVII,
3/2'5.28 Mevj furthermore a level with (15/2)" and, the,'eneigy &,5 Mov- i'b
d
us.. -of
*umedo, The relative probabilities for'varlio" types treizisitions. are
estimated from the relation between the 1 ifetime of a nucleus in~the-
excitecl state and the transition energy. The rimental and theoretical
'results are, in- good agreementi, Ther authors ~h!nxkpeffiV; Nikitova' for 1:aaf!~+
V.1% Sakharovj, B.S.' Dzhelepoyl- L
stance-in the-experiments.,* 4K0 Pek,
'N.N,i Fl,eroyj T.1f. -Tali tsyn,. A.B. Migdal#, L.T.'Groshe'v and I.S-; Shap'iio'.
are mbntioned. - There are 1 -figure an4,26 refe:rf?ncje9,s 8 'Soviet-bloo."'and
20 non-Soviet-bloo. The 2 most recent.references to English-languagp,pub-
lications read as follovBt D.,Strz)minger, J.M.''Hollander, G.T. Beaborg,"-
eata ;14

S/056/61/040/003/006/0~1
Study of the reactions,.p BIOIJB~02
Rev. Modo Phys, 3_0t 585t 1958; V.J* Aeby et al,,, Phya, Rove Lti fil 6p 1,958.
4SUCTATIONi, Institut*khimichaekoy fiziXi AkAdembi nauk SSSR
(Institute of Chemical Physics of t1he Academy of
Scibnoeo 'USSR)
SUBMITTEDt, October 7p 1960
Card,4/4

L 23 w(x)/vr(c)1WP(j)1T Pc4VPr.4
ACCEGSfOX 11H- -AP5003840 6/0190163/007/001/0180/0180.;,
AUTHORt Adadurov. 0. A. Barkalov. 1. VAJ Drool*,*
A !_ ~N' Inatovich, T. N,- Tal ros,!, V. L. Tq!7L0Tr_ "
P.
A.
k
TITLE: The phenomenon of ol meritati In a shoe ways
SOURCE: Vysokomolekulyarnyye soyedineniya, Y. 7, no. 1, 1965, 18o
TOPIC TAGS: polymerization, shook w&vo, mothaerylamide, trioxane,
explosion, polyoxymetbylene
ABSTRACT; A study has shown that a monomer in the condensed state
can be made to polym 0 by passAng a shock wave through it. Pow-
dered methacrYlamideIrn'd trioxane' Ivere palletized and sub4ected to
the action of a shock vaye with a vaye front pressure of 1.5-3 x 10
atm abs produced by the explosion of trotyl-boxogen. The temperature
in the pellet-containing capIU3 Immediately after the explosion did
not exceed 50C and dropped to 1,om temperature In a few minutes,
Mothacrylamide formed a polymer decompoolffs at about 2TOC Vith a
Card 1/2

L 23593-65
ACCESSION NR: AP5003840
yield of 5% on the monomer. In trioxans the polymer yield vas 3%;
the polymer behaves similarly to polyoxymothylons. Studies of poly-
merization in a shock vave are planned for other monomers. (SKI
ASSOCIATION: none
SUBMITTEW 24JunA ZNCLt 00 SUB.CODEj OC, MS
10 HEY 60vt 001 OTHERS 000 ATV PREGSt 3171
Card 2/2

ADADURO'l G.j..; BARKALOY, I.M.; COLIDAUSHY, V.I.; riREMIN, A.U.;
161ATOVICH,
T.N.; 141MAYLOV) AOL; TAJ,'R(-,ZE, V.L.; YAMPOLISKUY P-1.
Polymerization of condenced ircriomm In a -1.hock wave, Pokl-
AN SL~-TR 165 no.4:851-854 D 165. (FaRA 18:32)
L insLitut khimichenkay fJ-iki AN SSSR, 2.,Chlen-
korrespondent AN SSSR (for Golldanskiy)s
2

L 17629-66 RUM,
ACC M AP6001732 SOURGE.CODE: UR/0020/65/165/Oolj/0851/0854
AUTHORii Adadurov. 0. A ~kalov ~1. H. in, A.- Nei
,; Dre
Mikhaylov, A. N._j Tallrozo YOM Wkkiy, P",j Golf dansKizl_~I L_
-Mo-Fiebponding-memb(jr AIN SM
ORO: Inst itute for Ghomical Physics Academy_of SciancesiSSSR (Institute
khimiches oy fiziki AkademiiM__Uk__ R
TITLEs Polymerization of condensed monotners-in shock waves
SOURGEs AN SSSR. Dokladys Yo 165# no# h, 1965#'851-654
TOPIC; TAGSt polymerization, shook
wave I monomer
,pomore (trioxano,
ABSTRAM Ple.shock wave polymerization of condensed mo
agry dq, jKtassium acrylate) mothacrylamide, tolane, /ealicilic aldehydox
j~
otilbenes= di ho lbutadieno)lwas studied. T Sexpsrimontal technique followod
that dose bed 0. A. Adadurovi dr, (V,,rookomolek. soyed., 7 No. 1, 180, 1965).
The Werimental results are tabulated, A, is concluded that observed polymer-
Card 1/2 678.?4h; 534.222.1

L 17629-66 0
Arr, NRI Ar6oO1732 not due to 580orldary effeatao
directlY in the shock Wave and is
ization occurs 1 table. oo5
Orig. art, hass OOS/ OTH RU I
SUBM DkTz, oijun65/ ORID W'
SUB rOD]gt
Card 2/2
`F' F, 'Al
-R.
"U"
NK

L 40151-66
iACC NR: AP6012182 SOURCE CODE: UP,103861661003IC081030910312~'
Ta
AU1111011: B4jhLj()v I _11roze V. L.; Y iv A i
1. M. Gol IdansL W
s SSSR (Institut khimiches-
ORG: institute of Chemical Physics' Academy of Science
koy fiiiki demii nauk SSSR)
TITLE: intensification of a shock 'wave by the polymerization energy and the
feasibility of a -polymerization dertonation,j
SOME: Zhurnal eksperimentallnoy i teoreticheskoy fizjhi,---J4aJ edaktsiyu.
ed
Prilozheniye,, v- 3o no. 8, 1966) 309-312 VILE
on a ~ex
Ion'
TOPIC TAGS: shock wave interaction, chemical e Ion onp plastic explo ive) poly-
P1 plo
merization kineticap detonation) monomer JUL f? 0
Ln
ABSTRACT: Ibis in apontinuation of earlier wo (poki. Av sssR v. 165,, 851,, 1965)
0
V.~65" 8
(
n Jhe
where polyme ization/of several sho VdAy edp and
solid monomer
D;
eA
the energy release was estimated. In ihe pre:e a-authora compare this
e a result
energy with the energy obtained by the substance a a result of compression by the
shock wave. This is done by obtaining the dependence of the specific volume of
the substance on the applied pressure from the shock adisbat of the investigated
substance. The estimates are made for acryl amide, which was used in the earlier
studyt making use of published data on plexiglass and polystyrene, which have the
6, C

..L -4oi,51-66
ACC NR: AM12182 57
same initial density and approximately equal compression coefficlents. Since the
passage of the shock wave left no traces of melting of the substance it is con-
eluded that a considerable portion of the thermal energy released at the Instant
of polymerization-lit transferred to the shock wave, being converted Into elastic
energy of the substance. It in also shown that the energy released during poly-
merization is approximately equal to the energy lost by the shock wave to the com-
ession of the monomer. Therefore the additional fraction of the energy obtained!
r
P
by the shock wave from the chemical processes is comparable 9writh the total energy
obtained by the substance upon compression by the shock wave. From a detailed
theoretical analysis made by N. M. Kuznetsav at the authors' request (zhETF v. 49
Y
1526, 1965) and from other considerations it is conckuded that a detonation cah~
occur'as a result of polymerization by a shock vave. The authors thank Academician~
N. No Semenov and N. M. Kuznetsoy for a valuable discussion. [02)
SUB CODE.-Oj7.26 SUBM DATE: 17Feb66/ ono mn oo5/ OTH W.- 002:,-.,,- -
ATD PRESS:
Car 2/2 11b

ACC t"' APGO12921
WW(M
~T(m)/CWP(J) IJP(c) WIRM
SOURCE CODE: UR/0020/66/167/005/1077/1078
AUTHOR: Barkalo-,r, 1. M. -. GolldanBkiy, V.I. (Corresponding member AN MR); 7(7
Custov. V.V.; Dremin, A.N.; Mikhayov, AM,; Tallroze. V.L.;Yampo 'Liy P.A.
ORG: Institute of Chemical PhYSICB, Academy of Sciences,SSSR (Institut khJmfcheskoy
fizlki Akademii nauk-999TIT-
TITLE: Shock wave vulcanizatiod of rubbers
SOURCE: AN SSSR. Doklady, v. 167, no. 5, 1966, 1077-1078
TOPIC TAGS: vulcanization, rubber, shock wave
ABSTRACT: Continuing the study of ~olymerlzation in sh9t'.~ the authors investigateA
the possibility of yulcanizing rubbers by use of a shock wave. Samples of-U&II 5KDJr
r
I:nE-oBr-cca�o-q)~SKS-30AI,;ISKD, and polyisobutylene)~Tubbers were subjected to Lqhock waves
with amplitudes from 30, 000 to 100, 000 r1m. The percentage Of the gel fraction and Lhf,
molecular weight of the network were determined In each sample. No cross-linking could
be detected in polylsobutylene (a rubber having no doub!c bonds in the macromoleculc);
only a certain degree of degradation took place. The sho ck-wave- induced cross-linking
reaction in SKB rubber has a definite threshold character, the threshold pressure being
about 36, 000 atm. The gel fraction appears above this pressure, and at 80, 000 film tin
almost completely cross-linked vulcanization is obtained. A partial calcination is observed
above 100,000 atm. The vulcanization phenomena observed occur at the Instant the shock
r.,A 1/2 UDC: 641.12.034.2

L ~4041-66 - -------------------------
ACC NRi AP6012921
a time of the order of 10-6sec. Thusp in SKB
wave passes through the rubbeip L e. in atm in the shock wave, over 1019
rubber (MW 80, Ooo - 200, 000) at a pressure of 50, 000 gure and I table-
formed per gram in 1o-5 sec. Orig. art. has; I fl
cross-links are
SUB CODE: 11, 07 SUBM D.AT,E; 16Nov66 ORIG REF: 003 OTH REF. 001.
Card 2/
EN I
ll-l--I'----,v-` ,, W
'A

'ACC'_NR17 COD.E-_ UiVO06�1661O_iVO041O2621O2661
AUTHOR:
',~#.#ki,Yj,_ A.; KokarMin, V. F.; Golubkov.. A. 1#; Kondurushki if. A.;
Bolyatko; A. V.,
ORG: none
TITLE: Passage of neutrons through air
SOURCE: Atomnaya energiyap v. 21., no. 4., 1966,, 262-266
TOPIC TAGS: neutron radiationp radiation hazard., airL, neutron.interactionj neutron
anargy distribution) mdi&tion daaimtry
ABSTRACT: With an aim at reducing the radiation hazard to persons operating close to
neutron sources, the authors present a Monte-Carlo calculation of the neutrons from
monoenergetic point-like isotropic cources in an unbounded homogeneous medium of
known density. The initial neutron energies considered are 0.001, 0.025,, 0.21 0.8, 2.,
5, 10, and 14 Mev. The calculation was made with an M-20 electronic computer. From
7000 to 20 000 neutron histories were traced from the specified Initial energy down
to 0.2 ev. All possible neutron interactions with the nitrogen and oxygen atams in
air, contributing not less than 3% -to the total neutron cross section, were taken Into
consideration, and other impurities in the air were disregarded. The space-energy and
time distributions of the neutrons are obtained for distances 10 - 1Y')0 m from the
source and are presented in the form of numerous plats. Plato are also presented of
the average time necessary for the neutrons to reach a given distance for different
Ca,,d 3/2 UDC: 539.125-52

ACC NRt Ap6034092
initial neutron energies, and the flux'of neutrons with energies larger than 0.2 Mey
in air from point sources of various energies; and the neutron done from a point
source in airs The calculated neutron dose is compared with the experimental data
obtained by the authors and by others.. ~nd agree within 25%. Me authors thank 0# Is
Leypunskiy for twofal discusaiona. OrIg, art, ban: 12 figureas
SUB CODE.- 18/ SOM DATE: 18my66/ ORIG RU: 0051 OM RUI
Card 2_

YL'.'FC.-L'SXIY, P. V.
42307: Y-AMFCL'SXJY, P. V. - S-5-1--mai nrpl-t~r imifnat' -9 Vypolneniver pl-n-! E_-c,
nefti. Azerbsy4zh. nr;ft. T-t7cz-vr.;, 194,?, ~,,o. 10, v,- '17-19.
SO, LetoDis' Zhijrnql'nykh St-.tey, Vol. 47, 1948.

114 -.1 - 3/15
AUTHOR: Trifonov, E. V., Engineer and Yampollski, S. L. Eng.
TITLE: The Effect of Oil Pressure on the Load Carrying
Capacity of Steam Turbine Thrust Bearings (Vliyaniye
davleniya masla na nesushchuyu eposobnost' upornykh
podshipnikov parovykh turbin)-
PERIODICAL: ENERGOMASHINOSTROYENIYEj 19571 No. 1, pp. 8-11,
(U.S.S.R.)
ABSTRACT: The article describes tests on thrust bearings of the
Mitchell or Kingsbury types. The testing set-up is
illustrated by drawing in Fig. 11 po 8. Fig. 2$ p. 9p
shows the distribution of the metering points. Fig. 3,
P. 9, illustrates the pressure epurod along the radius
of the,thrust disc. The obtained 'results are described,
plotted in graphs (Fig. 5, P. 10) and entered in
Table 2, p. 10, On the basis of this, it Is concluded
that the load carrying capacity of high speed thrust
bearings (uav greater than 45 im/see, n = 5 000 - 10 000
r.p,m.) is governed primarily by the oil pNssure at
Card 1/3 the inlet to the thrust pads. Under actual operating

114 - I - 3/15
TITLEt The Effect of Oil Pressure on the Load Carrying
Capacity of Steam Turbine Thrust Bearings (Vliyanlye
davleniya masla na nesushchur sposobnost' upornyV-h
podshipnikov parovykh turbin
conditions this factor predominates over the influences
of the geometrical shape of the *pads, the smoothness of
the surfaces, oil temperature, etc. It is because the
effect of oil pressure has not been taken into account
that some bearings are of poor reliability and have a
low load carrying capacity. Depending on the type of
bearings and the conditions required pressures range
from 0.5 to 10 kg/cm2.
There Iare'four figures, one graph and two tables. There
are two Slavic and one Swiss reference.
ASSOCIATION:
Card 2/3

114 - I - 3/1;
TITLE: The Effect of Oil Pressure on the Load Carrying
Capacity of Steam Turbine Thrust Bearings (V11yan1ye
davleniya masla na, nesushehuyll sposobnost' upornykh
poduhipnikov parovykh turbin
ASSOCIATION:
PRESENTED BY:
SUB14I t
AVAILABLE: Library of Congress
Card 3/3

F
yg/)/~Z- t. L
TRIFCNOV, Ye.V., inzhener; TSUKANOV, V.F., Inzhener; YAMPOLISKIT, S.L.,inzhener.
Radial-tbrust bearing for at~-,i&2 turbines plAced with the oil pump.
Inargomashinostroenis 3 no.6:1-5 Je '57- (MIRA 10:7)
(Steam turbines)

I
-AUTfi0R-.--Trif onov-",-i-V. -;Engineo and
L'skiy, S.L., Engineer. 114-6-1/11
VITTS: Steam turbine support anO thrust bearing combined wi-th oil
pump. (Opo3mol-upoinyy polshipnik parovoy turbiny sovmesh-
chennyy s maslyanum nasosom.)
PERIODICAL: "Energomashinostroaniell (Power Generation Machinery
Construction), 1957, Vol- 3, NO# 61 ppe I - 5 (U.-.S.R.)
ABSTRACT: Steam turbine thrust bearings are one of the most com-
plicated and least reliable parts of the set. High speed
thrust bearings are particularly unsatisfactory. The Kal-
uga turbine works developed and have since 1954 applied a
new desiga of thrust and support bearing combined with the
main turbine oil pump. The special featU-TVB of this bearing
are that: 1) the runner of the centrifugal oil pump,
located on the front end of the turbine shaft, serves as
the thrust disc; 2) the front.suppoxt bearing of the
turbine also serves as the pump gland; 3) both support
and thrust bearings are lubricated by oil at high pressure,
since both are located in the pressure chamber of the pump.
The construction has been described in detail in an article
by N.M. Taranenko. A fairly detailed description with
Card 1/4 sketches is given in this article. Special tests on a
W=i

Steam turbine support and thrust bearing combined with oil
pump. (Cont.) 114-6-1/11
pump-bearing are described. A special test rig was set up
with a loading machin driven by an electric motor, oil
tank , filters and coolers and an auxiliary centrifugal
oil pump. The oil supply conditions in the turbine set are
carefully reproduced. Special investigations are being
made into the hydraulic part of the pump-regulator and are
not considered in this article. A disadvantage of the test
set-up is the limited load carrying capacity of the loading
bearing, therefom in making overload tests it was necessary
to reduce the number of thrust pads on the bearing being
tested. During the test the temperature conditions were
studied. The following were measured: 1) the oil press-
ures in the inlet and diaeba3Zge chambers and beyond the
pump Yunner and in the thrust bearing oil filml 2) the
oil temperatures in the inlet and discharge chambers, at
inlet and discharge from the thrust bearing and the temper-
ature on the thrust Dad surface and in the oil film;
3) the output of the pump and the quantity of oil passing
throueh the support bearing. The main results of the tests
are given in a table and also in a graph of the temperature
distribution on the surface of the bearing pads as a function
Card 2/4 of the specific load. A series of tests was made to deter-

Steam turbine support and thiust b&-ar-iii-g-c-ombined-with--oi-l-
pump. (Cont.) n4-6-1/n
mine the load carrying capacity of the thrust bearing. The
tests were continued to destruction of the bearing. Some
tests were also made to determine the limiting load when
the thrust disc was damaged. The specific-loads obtained
during the tests were high, evidently because in high speed
thrust bearings there is a zone of local low pressure,caused
by the pump effect of the disc and the presence of intense
turbulence. In ordinary bearings because the lubrication is
at low pressure this pressure reduction can lead to the
formation of vacuum zones in which bubbles can be fonaed.
In the present type of bearings this is avoided because the
oil supply is at high pressure -
The magnitude of the axial displacement of the rotor in
the event of accident was investigated.. The usual bearincr
0
gives considerable axial displacement when damaged. Because
high oil pressure is used in the present bearings other
bearing metals can be used which give less displdeement than
babbit in the event of accident* In particular brass proved
very suitable.
The system of having the support and thrust bearing
Card 3/4 directly in the chamber of the main oil pump was found to

Steam turbine support and thrust bearing combined with oil
pump. (Gont.) 114-6-1/11
ensure very reliable oil supply,
The use of tombined pump and bearing gives reduced
mechanical losses. Tests on turbines type AK 4-3 gave a
reduction of 12.? kW. For turbines running at a speed
higher than 3 000 r.p.m. the difference warj in some cases
20 M
The works carried out observations on the opeintion of
bearings of this desiga on two turbines in service which
have now worked for 6 000-9 000 hours. These sets worked
under the mot varied conditions including freqCient water
hammei7 and brief emergeucy interruption of oil supply.
Inspection after a year's operation show-ad the bearings on
both machines were in excellent condition. In additiong a
large number of turbines with bDarings of this type have
passed acceptance tests on the works test bed, It is con-
cluded that thesebearing-pumps have the advantages of much
higher and more stable load carrying capacity, reliable oil
supply, 'iigher efficierey, simpler construction and smaller
size
Ther~ aze 4 figures, 1 table'and 4 literature references
Card 4/4 (Slavic).
AVAILAATE:

104-3-6/45
AUTHOR: Trif onov, 3b. V. and Yampollskiy,'.S.P., Englneers.
TITIE; The measurement of axial stresses a steam turbine.
(Izmereniye osevykh usiliy v parovoy turbine)
4
PMIODICAL: IrElektricheski.Te Stanti ii" (Power Stations), 1957,
V01.281.No-3t PP- 19 - 21 (U.S.S.R.)
ABSTRACT: Existing methods of measuring axial stresses in steam
turbines suffer from a number of defects. Special spring
supports are required in the thrust bearing if it is intended
to use resistance strain gauges and so this method is mainly
used for large turbine sets. The method of measuring the
temperature on the bearing pads that is sometimes used is not
always applicable as is demonstrated by experimental curves
which show that the linear relationship between tempevature
and load which is usually adopted is only valict at a partic-
ular speed and over a narrow load range.
Accordingly a method was developed to measure the axial
stresses in steam turbinus from the pressure of the oil film
in the thrust bearing. The relationship between the maximim
pressure in the oil film and the thrust on the pad was calcu-
Card 1/2 bated. It is in practice convenient to measure the pressure
in the so-called 11centre of pressure" of the pad. A theoret-
ical basis for this method is given. Tests were made on two

1 104-3-6/45
The measurement of axial stresses in a steam turbine. (Cont.)
kinds of pad. Small holes were made in the face of the pad and
led to manometers through copper tubes which are sufficiently
flexible to permit movement of the pad. Ordinary manometers can
be used as great accuracy is not required. 'The results of the
tests are shown in the form of a graph and show some divergence
from values calculated from existing theories. Measurements
made in this way may be used for other purposes surh as for
checking the operation of compensating devices of thrust bearings
which should ensure even distribution of the load between the
pads and an example of this kind is given.
The comparative simplicity of the measurements and the uni-
versa.lit,y of this method for all designs of thrust bearings make
it possible to use it for investigation of the operation of thrast
bearings in operating conditions and for the adjustment of steam
turbines in cases when the strain gauge method cannot be used for
one reason or another.
There is an editorial note that until further experience has
been acquired the method can onl-y~,be recommended for turbines of
less than 25 MW- There are 5 fi~;ires and 2 Slavic. references.
AVAILABLE: Library of Congress
Card 2/2

TRIFONOV, Ye,V., inzh.; TAMLISKIT. S.L., lnzh.
Seleotion of materials for shoes in stream-turbine thrust bearings.
Energomashinostroanis 4 no-3:15-19 Hr 158, (MIRA 110)
(Bearingr (Machinery))

TRIFOROV, Ye.Y.,insh.; YAMPOLISKIY, S.L.,Inzh.
Temperature conditions in steam-turbine thrust bearings and
dependability of their performnnee, Iglek.sts.29 n0.3:23-27 Kr '56
(Bearings (Machinery) (MIRA 11:5)
j,"q
4,
Z

TRIFONOV, Ye.v., inzh.; YAMPOLISKIY, S.L., inzh.
Increase in ths reliability of the axial tx:arings of steam turbines.
Elek. sta. 31 no.9:27-30 S 160. (MIRA 3j,:10)
(Steam turbines)

S/122/63/000/003/004/OCO
A004/A127
AUTHORS: Trifonov, Ye.V., Candid ate of 'Technical Sciences,,_nip_2~~,
Khomyakov, V.P., Sarapov, O.P., Engineers
The effect of some design parameters of segmental slide thrust
TITLE
bearings on their efficiency,
PERIODICAL: Vestni k mashinostroyarLtya
no- 3, 1963, 20 27,
TM: The authorz give an account of experimental inveztigations per-
formed at the Kaluzhskiy turbinny Izavod (Kaluga Turbine Plant) on tilt-ing-pad
thrust bearings which were aimed at elucidating the dependence of their carrying
power on some design parameters which are not taken into consideration by the
universally adopted calculation methods. The bearings were tested at speeds of
30 - 70 m1sec, which is characteristic of steam and gas turbines. The main fea-
tures of the tested thrust bearings are presented in a table. The major purpose
of the testswas to determine the magnitude of the bearing breaking load under
various operation conditions and uf different designs of segmental thrust bear-
The following factors were'investigated; effect of the number of tilting
Card 1/2

3/1 2216,71WO03160;,100A
27 ---- - --------
iLds 1, geo -trical shape
. on the functioning of the thrust bearing,-pad materia ma
p
:of the pads, and effect of the sliding speed on the carrying power or thrust
-bearine.s. The authors present a detailed description of the tests concerning
the factors mentioned and give a number of recommendations in designing thrust
bearings of the type tested. There are 7 figures and 2 tables.
Card P,/ 2

1,RljS IjLyAKOV, V.P.; BEREZ11111SKIY, A.I.; SPIVAK, 14.Ya.; FINOGEi"Vl I.A.;
LIPETS, A.1j.; AYME711 B.G.; 'KOSTO7Y'ET3XIY, D.L.; BOLDZT;It K.I.;
[4lOTlb'Kjy '8.L.; "rEDOTOV, D.K.; Kl"lllLlM'j I.!.' OSf'_,t.T'G'V, 5-Ya.;
ki
y
WtOBLIN, G.A.; KAHATM, A.A.; BUIEGA, S.S.;
W~WYHRAN, V.A.; IOELISON, V.I.
Inventiona. Energ. i elektrotekh. prom. no.3:48-49 Jl-S 164.

YAMPOLISKIY, S.L., lnzh.
Effeot of operational and---daer.~gn 'factors on the rformance of the
thrust bearings of turbtnety methods for opej4t,'Anill ~-;, c-Ontrol and
damage protection. Enargomashl-no-stroinia 11 no.71l7-22 Jl 165.
(MRA 180)

ACC NR- A117007593
SOURCE COD[-*-. Ult/0104/66/000/008/0019/0022
A 0 T I 10R Vampol'okly, S. L. (Sszlno&r)
ORG: nolr~~~~
TITLE: Checking axial force In turbines by pressure in hydro dynamic
layer of miin bearing
8OURCE: Elcktrichesklye stantsii, no. 8, 1966~ 19-22
T011IC TAGS: turbine, hydrodynamic bearing
SUB CODE; 13
ABSTRACT: The Kiluga Turbine Plant devoloped a method for measuring axial
forces permissible for wide usage on turbines. Tills method is based on
measurement of the hydrodynamic pressure in the main bearing, and is do-
scribod In detail elsewhere. This article p:~osants a description of ey.-
porimantal testing ot tho bydrodynaptic pro!;sura in tho maLn boarines ot
three widely used typos of main bearings. The experiments were performed
on a special loading machine alluding the application of various loads
to a bearing being tested under condition5 near actual usage conditions.
Graphs of the variation of pressure at the main bearing as a function of
load are prcosented. The graphs are near linear over a wide range.
Checking the hydrodynamic pressure In the nain bearing Is a valuable oxpzrimen-
tal means of checking usage chaaractorllsti= defining the state of the
operating process In the bearing, as the prcsonco of hydrodynamic pressure
in tho bc!aring Indicates fluid frictiont without which the main bearWr
cannot operate. OriZ. art. has: 3 figuras and 2 fomulas. Ljpi~a.' 38,3.!Y
1/1
UDC: 621.165

L 2030-66 34T ('M)/EPF (c)/LWA(d)/T/~A'
'P(t)/W(z)/a1P(b)/ff C(m) JDA-iWIW
'ACCESSION NR. AP5018372 UR/0114/65/060/007/0()17/007.Z
621.165.001, 5
7.
AUTHOR: 'Y!nkoll~kfy L!_(Engineer)
TITLE: Effect of design and operational factors on the operability of turbine
thrust bearingrsl\\ methods of checking the operation and protecting against failure
ol BearlngY-.1-1
SOURCE: Energomas.hinostroyeniyal no. 7, 1965, 17-22
TOPIC TAGS: thrust bearingi turbine bearing
ABSTRACT: According to varioun experimental datu, the bearing capacity of
Mitchell-type thrust bearings in high-speed (o
ver 3000 rpm) thermal turbines
ese- factors:
Design shoe (or segment) material
depends on th parameters,
(babbitted copper proved to be the best)i oil pressure;. oil flowl sliding speed; oil
scosity; alignment of bearing surfacesi bearing ~i
vi -surface roughnesel presence o i
abrasive particles. Static overloads of thrust bearings, when axial load exceeds.
bearing capaciti, can be detected, and the bearing breakdown prevented, by ~
monitoring the temptrature,of the shoe metal. However, most serious causes of
'[card 1/2
MR

L 203C-M
ACCESSION NR: AP5018 372
bearing failure (oil-pressure or rate-of-flow drop, air in the oil film, babbit
crumbling, abrasives in oil, dynamic overload) cannot be detected by monitoring
temperature; such conditions are accompanied by a collapse of the hydrodynamic
pressure in the oil film. 0 Hence, a new protective system for steam turbines has
been developed which continuously measures - through. a special channel In one oc
the shoes - the hydrodynamic oil pressure by means -of-a contact manometer.
When the oil film in the bearing is broken, the protective system shuts dow the
turbine and gives off an audible siZnal. Orig. art. bac 5 figures and I formula,
ASSOCIATION's noqe
SUBMITTED. 00 :ENCL;. 00- SU13 CODE:,
No REIF SO"Vi, 0 14 OTHER: 002

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Ood Wftslivn The I~k%l exproiriore of bulhilog so 1,Ig works for
Irrating 1~qhl alloM am discus--d. lXnvtbqw and Advitr am xivvn on th"
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NO 41 WilA

YAPPOLISKI f.9-s-e-
Voprosy skorostnogo proektirovaniia i osvoeniia novykh konstruktsii v mashino-
stroenii. Moskva., An sssR. 1944. 108 p. dingrs.
Bibliography- p. 106-107.
Problems of quick designing and the utilization of new designs in machine-
building.
DLC: T.1230-13
So: Manufacturing and Rechanical Engineering in the Soviet Union, Library
of Congress, 1953.

v ! I ~ , . f I. - ~ I I I "' - .1 - ~ ~
Techinical Education - flistory
History of the LIviv Polytechnical In:-Aituxe. Ilauk. zap. LPI No. 1, 19/.7
Monthly List of Russian Accessions, Library of Congress, December 1952. Unclassified.

)6POLISKII) S. M.
Skoi-ostnoe osvoenie novykh proizvodstv. Moskva, Mashgiz, 1949. 153 p. diagrs.
Bibliography: p. 153-154
Quick mastering of new production processes.
DLC: TS155.12
SO: Manufacturing and Mechanical Engineering in the Soviet Union, Library
of Congress, 1953.

Increasing Labor Productivity in Machine Building (Vol)rosy povysheniya
proiavoditellnosti truda v mashinostroenii) Gosudarstvennoye nauch-tekb.
izdat. mashinostroitell, literatury, "pscow, 1957. 511 pp.
(Table ofContents authors)/,/#-)
This collections pre:~ents a comparative tech. and econcmic analysis of
most effectivd metl~ods and industrial processes for obtaining bi~7:h labcr productivity
in machine building. Output may be step-.ed up by further standardization ff machine
tools, traterials, and production methods; drawing on unnsed potentials. -
Covers all sta,ves of pla nning and production as r:erformed in iiodern plant5 of
USSR, actual experience, and new methods are discus--ed.
YAAFOLISKIY, S. M., "Utilization of Production Reserves," P. 7.
. . . . . . . . . . .....
PW.
ATW

SAKSAGANSKLY, Toodor Davidovich; YAKPOLISKIY, S.M., kandidst okonomichaskikh
nauk, retsenzent; PAMILM61 rirli`~"'fedivktor; PROKOYIYZYA, L.G.,
radaktor Izdatelletva; TIKHANOV, A.Ta., takhnicheBkiy radektor;
ALIKININ, V.D., takanichaskiy radaktor
(Organizati,gn of production in machine manufacturing plants] Kak
organizovano proizvodstvo na mashinostroitallnom zayode. Izd.2-oe,
dop. Moskva, Goa.nauchno-tekhn.izd-vo mashinostroit. lit-ry, 1957.
226 p. (MLRA 10:9)
(Machinery industry)

S7/11.
3-58-3--7/32
AUTHORt Yampollskiy, S.M., Dotaent, Candidate of Technical Sciences,,
Director of the Odessa Folytechnical Inatitute
TITLEt On the Duties of a Dean (0b obyazannosUyakh dekana The Or-
ganizer of the Npartment's Scientific Work. (Organizator nauchnoy
raboty na fa-kultete)
PERIODICALt Vestnik Vysshey Shkoly, 1958, 141- 3, PP 30-33 (USSR)
ABSTRACTt With reference to Nr 9 of 1957 and Nr 1 Of 1958, this peri-
odical, the author deals extensively with the duties of a
faculty dean. The deans munt direct the varied activity of
the faculty, raise the students, cultural level, take an in-
terest in their welfare, and pay special attention to their
ideological education. Under present. conditions, the dean
Is obliged to Bee that the chairs of his faoulty coordinate
their scientific work more closely with industrial needa.
In the author's opinion, the deans must not oqly control
the course of research and exert influence in raising the
instructord' qualifications, but must also assume respon-
sibility for the condition of the work. The author mentions
here the Llvovskiy politekhnichaskiy institut (Llvov Politech-
Card 112 nical Institu fto) which, within a short period, succeeded
kin

3-518-3-7/32
On the Duties of a Dean. The Organizer of the Department' a Scientific Work
notably in these fields, because the faculty deans, and
especially the deans-professors K.B. Karandeyev, M.Si Koma.fov
and T.P. Gubenko systematically directed the scientific work.
The same can be said about a number of other vuzes. The author
emphasizes that both the organization of the teaching-
educational and of the scientific work of the doun are equally
importaht. The author then compares the ideological-political
education of the students as conducted at the Llvov Pdlytech-
nical Institute with that of the Odessa Polytechnical.Insti-
tute, where the deans are not in contact with the social or-
ganization and have refused to assist the Komsomol and Prof-
soyuz committees in organizing the student activity in arts,
sports, etc. The author states that the new statute of the
higher educational institution must state the dean's duties
and rights in plain terms. In the author's opinion the dean
should be elected and not appointed and the election should be
approved by the vuz director instead of by the blini3try. There
is 1 Soviet reference.
ASSOCIATIONs Ode8skiy politekhnicheskiy institut (Odessa Folytechnical
Institut)
LVAILABLEi Library of Congress
Card 2/2
.4~

YAMPO ollalkyi, S.M.]) Prof.; VETIGEROVSKIY, Ye 0. [Venherovalkyi,
IE.O.],, vrach; ABER, S.,a.', dotsent; SHELUDIKO, Ye.l. tSheludiko, IE.I.J,
viach; KHODOVAI R.Z., vrach
In memory of O.M.Fedotova. Pod., akush. i gin. 23 no.6:34 161.
(MRA 15:4)
(FEDOTOVA, OLENA RYKIIAILIVIIA, 1884,10W)

YAMFOL'SKIY,,P.M'.3 red.
(Ufle of regulated silicon rectifiers in controlled electric
drives and electric traction] Primnenie upravliaen7,kh krem-
nevykh vypriamitelai v reguliruemom elektroprivode i elektro-
tiage; referativnyi sbornik. Moskva, TSentr. in-t nauchno-
tekhn. informataii priborostroeniiap elektrotekhn. promyshl.
i aredstv avtomatizatsii, 1962. 54 p. (MIRA 1715)
1. Russia (1923- U.S.S. R.) Gosudarstvennyy komitet po avto-
matizataii i mashinostroyeniy-u.

OLENIN, A.V.; YAMPOLISKIY, S.M., red.; SKAKALISKAYA, L.N., tekhn.red.
[Use of regulated mercury rectifiers in electric locomotives]
Primenenie uprayliaemykh rtutnykh ventilei na elektrovozakh.
Moskva) 1963. 19 PO (MIRA 17:1)
1. Russia (1923- U.S.S.R.) Gosudarstvennyy komitet po elektro-
tekhnike.

YAKOBSON, N.B.; MWI-13HY, S.H.
[Use of silicon power rectifiers in electric drives;
from materials of the ASEA firm] Primenenie silovykb
upravliaemykh kremnievykh ventilei v elektroprivode;
po materialam firmy ASEA. Referativnaia informatsiia.
Moskva, Izd-vo TsINTL _1963. 23 p. (MIRA 16:9)
1. Russia (1923- U.S.S.R.) Gosudarstvennyy komitet po
avtomatizatsii i mashinostroyeniyu.
(United States--Electric driving)
(United States--Silicon diodes)

YAMFOLISKIY, S.M., doktor ekonomicheakikh nauk, prof.
Reliability and durability of machinery as economic factors.
Vest.mashinostr. 43 no.1s79-W Ja 163. (MIRA 16.2)
(Machinery-Industrial capacity)
N",
R

-Y IZ! F 5M,- 5,14 F k IT' i (
.,_prof.; ERLIKH, L.B., prof.; SHMIG L 1-Yu.,
dots., kand. tekhn. nauk, retsenZcnt
(Economic.s of mastering machinery of new design) Ekonom.'ka
osvoeniia novykh konstruktsli mashin. I-Ioskva, Z'-'~ashho-
stroenie,, 1964. 164 p. (IMIRA 18:2)
f

BAKHTINA, Te, A., YAMFOISKIY, To Q.) ilizhop BAZHENOVy Ve P., Inzh,, VEREVDI, F.P.,
Inzh,
Vaesoyuznaya Kontora Tipovogo Proyektirovaniya 1 Tekhnicheakikh Issledovaniy
MIS) Mintyazhstroya
Ventilyatornyye (Iradirid Page 53
SO: Collection of Annotations of Scientific Research Work on ConstrucLion, calpleted
in 1050. "oscm-1, 1951

BAKHTIMA, Ye, A.s Inzhener. is YAMPOLISKI-Y, T. S&I Inzhes VERIN, He F... Inzh,
Voesoyuznaya Kontora Tipovogo Proyektirov-aniya i tekhnicheskikh isaledovardy (KTIS)
Mintyazhatroya
SieteW mesnoy kanalizataii B polyami pddzmwy filltratBii (instruktoiya po
prove ktirovaniyu sistme) Page 60
SO: Collection of Annotations of Scientific Research Work on Construction, comnleted
in 1950. MoBcow, 1951

"EMOV I A . -1 or, t 3.% nL -7
Technology
Podzemnaia filftrat5iia stochnykh ,rod (Ur 4~.,rgrc-umd f!Itrat-*cn of sewage). Floskva,
Stroiizdat, 1951. 176 p.
2
9. Monthly List of Russian Accessions, Library of Congress, Novembur 1951. Unclassified.

NURABOV, V.G., lnzh.; YAMPOLISKIT, T.S., inzh.
Usine, precant reinforced concrete construction elements in
building cooling towers with ventilating systemn. Prom.otroi.
38 no.1:31-34 160. (MIRA 1315)
1. Treat Hooetroy Ho*4 (for Fokrasov)e 2. Giprotio (for Yampol'skly).
(Cooling towers) (Precast concrete construction)

YAMPOLISKIYp T.S.; ZOTOV9 G.V.
------------
[Catalog and handbook on cooling towers] Katalog-.Bpravd PO
gradirniam. Moskva, 1962. 109 p. (MIRAt)
1, Moscow, Gosudarstvennyy institut tipovogo i eksperimentallnogo
proyektirovaniya i tekhnicheakikh isaledovaniy. 2. Naeballnik
otdola promyshlennykh vodoprovodnykh aooruzheniy-qosudarstVennogo
institute. tipovogo i eksperimentallnogo proyektiz-btaniya
tekhnicheskikh iseledovaniy (for Yampol'skiy). 3. Otdel promysh-
lennykh vodoprovodnykh sooruzheniy Gosudarstvannogo instituta
tipovogo i eksperimentallnogo proyektirovaniya i tekhnicheskikh
iseledovaniy (for Zotov).
(Cooling towers)
------------------

ACC NRs AP7002203 SOURCE CODE: 3
AUTHOR: Yampollskiy, V.; Rzhevtsev, V.
ORO; Omsk PedagoGiedl Inatituteo Department of Physics (Omskiy
pedagogicheekly instltiit, kafedra fiziki)
TITLE: Determination of velocity of low-ionospliere vertical drirt
SOURCE: Geomagnetizm i aeronomiya, v. 6, no. 61 1966, 1116-1118
TOPICTAGS: ionosphere ionospheric physics., A0A1,&,rpyeR1e, D-VIF-r
ABSTRACT: The velocity of vertical drift of low regions of the iono-
sphere was determined using spectral analysis of' the field intensity of
radio waves in respect.to time. In order to determine vertical iono-
spheric drift velocity VV while taking into account the spherical shape
of the Earth, the following formula was derived;
x rhos + 4a sins "I" + 4) h
~'-7 0 1 ~ -FA,
14 + 2a sin"
gh
V, w
Card 1
UDC: 550-388.2

ACC NRj
where X is a wavelength of the transmitter; ho, an initial height of
reflection;,a, the radius of the Earth; 0, a central angle correspond-
ing to the half are between the transmitter And the receiver, and T,
a period with which the field intensity changes at the receiving point.
An experimental Investigation to determine Vv was conducted during the
solar eclipse on 15 Feb 1961 in four directions'with various equivalent
frequencies (feq,). To determine feq. a graph of electron concentra-
tion variations N) in the D-layer plotted on the basis of averaged
daily data obtained by rockets was used. Dependencies of ho on N com-
puted for every direction were plotted. Computed values of Vv are
shown in Fig. 1 as a function of N. Curves 1 and 2 show the values of
the vertical displacement velocity of regions.with various concentra-
tions during the first half of the eclipse and curves 3 and 4 represent
the second half. The assumption was made that the slight difference
between curves 1 and 3, and 2 and 4 can be rdlated to the spherical
shape of the Earth,, a factor which was not compensated for (curves 3
and 4 were plotted on the basis of data obtained by I. M. Vilenskiy and
B. 1. Podlipalin. Geomagnetizm I aeronomiya, 1964, no. 3, 417), and by
the fact that Vv data were determined for various ionospheric regions
separated from each other by several hundred~kilometera. The general
variations in the dependence of Vv on N seem;to be realistic because
the relative change.5 in electron concentration in low ionospheric layersi
are faster during the eclipse. Orig. art. has: 2 figures, 1 table, 7
and 1 formula. [WA-31 !

Fig. 1. Vv a,0a runction of N
.cm3 4w &v
I ISUB CODE: O)V SUBM DATE: 05Apr66/
OR;IG REF: 002
UAW-- - -
N -6-2'-
A
CC R AP70 203

Y, V,
FOIT-YUNG, I.Ye.; YAMPOLISKIY, V.13.
Diagnostic significance of the examination of bronchial lavage for
Koch's bacillus. Probl.tub. no.4:65-69 Ji-Ag 153* (KE.R.' 6:11)
1. 1z Llvovskogo oblastnogo protivotuberkulesnogo dispenser& (glavnvy
vrach - dotsent I.S.Befter). (Tuberculosis)

POVISOVSKIyt V.F.; KASTORNAYA, M.A. (deceased ];..UMFQL 1.SK,1-YJV"Y.. B.
Morphological changes in the brouchi in resected lungs from
patients and their relation to postoperative complications.
Probl. tub. 42 no.3:70-74 164,, (MIRA 18il)
1. Llvovskiy nauchno-iosledovatellakiy Institut titbarkulaza
(direktor G.I.Chemerlo, nauchnyy rukovoditell - prof. 1.T.
Stukalo) i L'vovs),aya oblastnaya protivotuberkuleznaya boltnitaa
(glavnyy vrach V.N.Kishakevich).

- I - i I i ' I I ~-' s J- - ~ j ~N - IL -1 - ft - -.. ~ - . - . - -- - - ---- - - -- - - -1 - - -- -
YiWL,UI0!'KIYp A. "I.; -VIZOLIJKLI, 1. 0.
Geometry, Won-Zuclidean
Some specific points concerning the interpretation of'Lobachavskiyls plane geometry., Uch.
zap. Xosk. un., no. 148, 1951.
~
2
9. Monthl List of Russian Accessions, Library of Congress, MaX -195~, Uncl.

firitennas and Transmission Lines 11)-:2535
rimpoLl ShIt. t-, (~'
d 1/1 fub. c0 - 3/12
Yampollskiy, V. G.
wM'&VbFY'f wv"9~' ~-!. ~:
Title : !.pproximation Method for Determining the Influence of Ph-use Dis-
tortions in the Aperture of a Spatial Antenna and Its Rad.Lation
Characteristics
Periodical : Radiotekhnika, 10, 17-24, MaY 1955
Abstract : Radia+ors in the form uf cophazally excited surfaces (para-
bolic, lens, etc) in practice never possess precisely co-
phaeal fields, due to imperfections. The Liuthor discloses
a method for approximate calculation of definite integrals
from the complex function of a real wariable. The method
give;; quite accurate results for subintegral functions with
a slightly varied phase. Radiation characteristics of Gpatial
(or linear) antennas under phase and =plitude distortions in
their apertures can be found by this procedure. Graphs, table.
One US Referencj.
In3titution
Subm
itted November 18) 1954
~717
14,

TAKPOLISKIY, T.G.
Inclined incidence of plain waves in a vira circuit. Radiotakhnika
10 no69:39-48 $155. (Km 9:1)
(Radio--Antennas)

I i z-

SUBJECT USSR PHYSICS CARD I / 3 PA - 1708
AUTHOR 1AMPIOLMlibl. -G.
TITLE The Reflection of a Plane Wave from a Wire Net at Normal
Polarization.
PERIODICAL Radiotechnika, 1-1, fase. 11, 33-37 (1956)
issued.- 12 / 1956
The reflection of a plane electromagnetic wave from a not conninting of wires
with a round cross section and equal spacing is investigated for the cane in
which the vector of the electric field of the impinging wave is within the Sur-
face of the net and is vertical to the axes of the wires. The diameter of the
wires of the net is assumed to be considerably smaller than the wavelength. At
first the problem of the diffraction of the plane wave with normal polarization
by a single conductor is dealt with. For this purpose the results obtained for
a thin conductor from the.works by IGNATOVSKY "Annalen der Physik, 1905,.L8,
fase-3 (1905) and by A.I.POTEHIN "Sovetskoe Radio,,, 1948, are used. A system of
polar coordinates (R,y) is connected with the conductor. An equation is obtained
from which it may be seen that the voltage of the secondary field is proportion-
al to the square of the radius of the conductor and is very low in the case of
thin conductors. Secondary radiation has a very marked character in one direction.
This is explained in the following manner: The analysis of the formula for the
current density J(9) on the surface of the conductor shows that, in the case of
thin conductors (Q 5 m.
are given for the radiaton pattern of the aa-,,e
antenna. A number of graphs represent- the radiation
pattern -for antennasoC length L = 1,000, 2,000, and
3,000 m, and for X = 200, 4oo, 8oo, and 2,01,00 !:,,.
It is seen from the radlation pattevn:3 in a vertical
plane of t1he antehnaaxis that the directional
properties of wave antennas suspended oveer humnid
ground are better than those of antennas ozer dry
ground. Expressicns (13) and (i4) are given for
parameters D and D' characterizing tho noiseproof
feature of the antenna. The expression for b.
characterizes the nolseproof featUre during the day-
tim~n whon on1y nurface waves a-o
2.:
Y vt
2.-
31 d 7 1 F; (A. ,I cm A 'd a
0 0

Traveling Wave one-Wire Antenna for 77-170"
Reception of Medium Waves SOV/108-1.5-1-2/13
HeveA is angle of elevation; is azimuth angle;
F(A,(P) is the radiation patte(A. D' was calculated
usJng numerical Integration of radiation.patterns.
Froin the plotted results it may be seen that for
X = 200-2,000 the length L of the antenna should
not exceod 3,000 ri, because in this ca3e the values
of D' diminish within the range of shoetev waves.
Expressions for tt,.e. amplification coefficient of the
wave antenna are given for the sky wave and the
surface wave. They contain the factor gr(L) whicn,
depends on the antenna lenpth L as shown by Eq. (18):
v,)
where Icl equials CL/4k = c/v. It muy be seen that an
optimuir antenna length Lopt may be obtain-7~d. An
approximate formula for Lopt is derived froin the
maximum condition for g(L). There are 11 figu7es;
Card 5/6 and 6 references, 4 Soviet, 2 U.S. The U.S.

Traveling Wave One-Wire Antenna for 77-176
Reception of Medium Waves SOV1108-15-1-2113
ences are: D. Carson, BSTJ. Nr 10, 19206; W. Wise,
PIRE Nr 4, 1934.
SUBMITrED: April 11, 1958
Card 616
_0

BEIDUSOV, S.P.; YAM IS G.,.otv. red.; VORONOVA, A.I., red.;
mmodl-J-K.- ., tekbn. red.
(Directional antennas for radio reception in the range from
200 - 2000 meters] 14apravlenrWe ai;tenrq dlia professional'-
nogo priema radjovesbehaniia v diapazone 200 - 2000 m. Mo-
skva, Goo. izd-vo lit-ry po voprosam eviazi i radio 1961. 71 p.
~IKIRA 140)
(Radio-Antennas)

31209
S/108/61/016/012/003/009
0 0201/D302
AUTHORSt Ayzenl)ergt G.Z., Beloueovq S.P*~ Lindebergg A.Kh., and
Yampo 1 $ a V. G. , Memb e r aof the Society$ (See Associa-
~t7~ 0 R J_
TITLE: An anti-fading broadr-ast antenna
PERIODICAL: Radiotekhnika, v. 16, no, 12, 1961, 21-30
TEXT; In the present article, the authors describe an antenna designed
so as to have anti-fading properties within a wide frequency band. The Wr
antenna is based on the wide-band anti-fading antenna with controlled
current 'distribution as suggested by G.Z. Ayzenberg in 1939 (Ref. 1:
Elektroavyazg, no. 9, 1940) (Ref. 3i Author~a certificate No. 71603
of December 12, 1948). Controlltd. current antennae, described recently
in foreign literaturt are dtaigned around the Ayzenberg principle# but
are not designed,for wide band operation. The wAtnny described is based
on the exteaded band w~,.dth 200-2000 m. rangt antenna as shown on Fig. 2~
It consists of the mas-tod insulated from earth. The screening of the
Card 1/4

An anti-fading
31200
S/1081/61/016/0.'2/003/009
0201/D302
feeder 2 is extended up to height H I around tht antenna mast. The current
in the antenna is controlled by mea:ns of a variable impedance in the form
of a s.c. stub, connected betwe.-,~n the earth and the lower end of the
screening. The see* sfiAb 1"r% attually thcL ouler sheath .3 of the feeder.
By changing tht length of the e.rs linD from 0 to ~,/2, the input resia.
tance varies from .-Ic-:1 t& to",. The rea,.A anss~ is controlled by moving the
s.4,*;. stub to earth 4. To decrbase surfate ;osses - a thick wire mesh
is placed under tht stjb a. Matching is eithor by a distributed or a
lumped constant transmIssion Ent. The main dimensions have been chosen
for the antenna to have aat~-f;ding properti*s in the 200-550 me band#
The htight cf tht antenna shoul 'd rot exceed 220-230 mg although to in-
creas^_ the band width at haa ae;tually been increased to 257 m, the
height of screening H I carz-taponding then to 0.33 H. Increasing H I to
0.5 H increases thr, cptrating down Ot- 140 m with better anti-fading
propeuties at 200-230 m. The impedantre of the antenna
depends*on the xran!Rm-~'tter power. The --haxacteriatic stub Impedance W.

31209
3/108/61/016/012/003/009
An anti-fading ... 0201/0502
may be taken as 60 -~ 120 oluns, with the maximum stub length 160-200 m.
Because the antenna in fcd not at its buse, but at a height 0.3 t 0.5 11,
its radiation pattern depends little on its characteristic impedance.
The following statements are made in conclusion: 1) The designed antenna
has good anti-fading properties. An intenna 257 m high has good direc-
tional properties in the 230-250 m range.. 2) Mien tuned to maximum
gain, the gain is substantially increased in comparison to that of anti-
fading tuning. 3) The experiments, carried out with a'scaled down
model of antenna, confirmed the results of theoretical calculations.
4) The controlled-current antennae should find application in new broad-
casting centers in the modification of existing antennae systems. There
are 10 figurss, and 5 references: 3 Spviet-bloc and . 2 non-Soviet-bloca
The references to the English-language publications read as follows:
H. Brueckmann. Electronics, v. 23, no. 3, 1050; 11. Page and G.D. Mon-
teantf PIEE, part 3, v. 102, no. 3, 1955.
ASSOCIATION: Nauchno-tekhnicheakoye obshchestvo radiotelchniki i
clektrosvyazi im. A.S. Popova (Scientific and Technical
Card 3/4
'Y

31201~
S/108/61/016/012/003/009
An anti-fading.... D201/0302
Society of Radio Engineering and Electrical Communications
im. A.S. Popov) CAbstracterlt4 note: Niww of Association
taIcen from first page of journaD
SUBMITTED: May 30, 1961
Card 4/4
2
Fig. 2

2, /700
37571:
S11 06/62/0w/005/r,03/007
A055/A101
AUTHORSt, Belousov, S.P.; Yampollskiy, V.G.
TITLE: Two-wire traveling wave antenna
PERIODICAL: 'Elektrosvi(azly no. 5. 1962, 24 - 30
4
TEXT; In this article are examined the parameters of a short wave two-
wire traveling wave antenna installed over a damp ground. The parameters of the
medium wave and long wave antennas were discussed by the authors in an earlier
work "Dvukhprovodnaya antenna begushchey volny" ("Two-wire traveling wave an-
tenna )". Sbornik NII Ministerstva svyazi, 1960, no. 2, (16)]. In the first part
of the present article, the authors reproduce a formula giving the efficiency
coefficient m as the ratio of the gain of a two-wire antenna to the gain of a
-he same length. They also reproduce a formula giving
single-wire antenna of 4. 4
the radiation pattern of the two-wire antenna. In the second part of the arti-
cle, they deal with the propagation constants of the current along the single-
wire antenna (*y 1 - dl - i A,) and the two-wiro antenna 2 d2 i These
constants are determined by the following exprozoionst
Card 1/3

S/Io6/6VOO0/005/003/G07
A055/A1O1.
Two-wire traveling wave antenna,
RI (6), and I R2
2h 2h (7)
~n cc In
where h is the suspension height, is the radius of the wire, and
S2 w 1/ 1112 + off - W -bw.
R1 r 0 dw
1 I/w2 _+P2
0 W +
CIO
R2 S2 W - IfIv2 _+P2 _ W -bw ~os awdw, (9)
Tr W + 1 -j
,-iher ' 7 1~ ~v+ p2
e 6-1 is the complex permittivity of the ground, and s Y-I'-01' (10)
b = 2 0(, hs (11), a - o~ ds (12), p = "/I S_ ' (I PI - 1).(13~
The authors describe a new method for computing the integrals in (8) and (9).
These integrals, as computed by this method, give a more accurate-formula for
Card 2/~

Two-wire trave'ling wave antenna
S/106/62/000/005/003/007
A055/A1O1
the calculation of the current propagation constant (in the short wave range)
than the asymptotic formiula deduced by Wise ("Propagation of high-frequency cur-
rents in ground return circuits", Proc. ME, 1934, April). In the third part of
th e article, the authors present three graphs showing the dependence of the cur-
rent attenuation constant upon the distance between the two wires for three dif-
fergnt wavelengths. They also give graphs Bhowi,.ig the phase velocity of the
current. The analysis of the 'Uhus obtained data leads the allVnors to the con-
clusion that the efficiency coefficient m, characterizing the gain ensured by
the use of a two-wire antenna, possesses the following properties:
W1 W
m ~:o 2 (25), m 1-,2 (26)
W,
A__4 0TI-10. %__J~ 4.
W, and '~42 being, respectively, the wave impedances of a single-wire and a two-
irire antenna. T"he efficiency of the two-wire antenna was also determined exper-
imentally; the experimental results are in good agreement with the calculated
ones. The So7iet parsonalition mentioned in tho article are: G.Z. Ayzenborg,
G.A. Grinberg and B.E, Bonshtedt. There are 9 figures and 8 references: 5 So-
viet-bloc and 3 non-Soviet-bloc.
SUBMIMED; December 20, 1961
Card 3/,3

Yk)4P0I-9XIY x V. G.
PHASE I BOOK EXPLOITATION SOV/6112
Ayzenberg, Grigoriy Zakharovich
Korotkovolnovyye antenny (Short-Wave Antennas). Moscow, Svyazlizdat, 1962.
814 p. Errata slip inserted. 10, 000 copies printed.
Rosp, Ed, -, G. N. Kocherzhevskiy; Tech. Ed. -, G. I. Shefer,
PURPOSE: This monograph is intended for scientists and radio engineers con-
cerned with the theory and design of short-wave transmitting and receiving
antennas. It may also be useful as a textbook for students in advanced radio
engineering courses in schools of higher education.
COVERAGE: The present work is a revised edition of a book by the same author,
entitled "Antennas for Main Short-W-ave Radio Communications, " published in
1948. In the new book considerable progress in the field of short-wave antennas
is taken into consideration, and the latest developments in antenna technique,
I_&-
Card I/ ap

Antennas (Cont.) .
SOV / 6112
such as cophnsnI band antenna nrrnys with parasitic reflectorn, traveling Wave
nntennas with pure coupling resistance, logarithinic antennas, and band shunt-
fed vibrators, are described. The chapter on rhombic antennas is substan-
tially expanded. A new chapter (XVI) dealing with single-wire traveling wave
antennas is introduced. The fundamental problem of the interference immunity
of various recei%ring nintennas is discussed In an added chapter ('XVII), Ch. XIII
was written by S. P. Belousov; Chs. XIV and XV, by Belousov and V. G.
_Yapjp~~~ Ch. X-VIII, by 1- K. Olifin; and Sec. 4 of Ch. )UX, by AL A.
Shkud. The graphs for calculating mutual impedance in balanced vibrators of
arbitrary dimensions were compiled under the supervision of Belousov. The
author thanks the coauthors and L. S. Tartakovskiy, Ye. G. Pollskaya, V. G.
Ezrin, 1. T. Govorkov, and G. N. Kocherzhevskiy. There are no references.
TABLE OF CONTENTS:
Foreword
List of Basic Symbols
Card 2/40
11
13
q`iil!~ Liz
0

Antennas (Cont. ) -
13. Bent rhombic, antenna
14. Suspension of rhombic antennas on the common poles
15. ' Structural performance of rhomble antennas
16. Receiving rhombic antennas
Ch, XIV. Traveling Wave Antenna
1. Description and conventional symbols
2. Traveling wave antenna principle of operation
3. Optimum phase propagation velocity
4. Selection of coupling elements between the vibrators and
collecting line
5. Calculation of phase velocity v, attenuation Oc , and
characteristic impedance W of the collecting line
6. Formulas for directional pattern of traveling wave antenna
7. Directivity factor, gain, and efficiency
8- Complex traveling wave antennas
Card 4102;
SOVI 6112
456
464
468
473
478
480
483
490
492
494
495
498

Antennas (Cont.)
SOV/6112
9. Electric parameters of traveling wave antennas with
resistance coupling
10. Traveling wave antennas with controlled directional patterns
11. Directional properties of the 3BS2 antenna (complex traveling
wave antenna consisting of three BS2 antennas) :-120
12. Directivity factor, efficiency, and gain of the 3BS2 antenna 2
13. Electric parameters of traveling-wave antenna with capacitive
coupling elements 5 3 6
14, Phase shifter for steering directional pattern of the 3BS2 antenna 553
15. Vertical traveling wave antenna 555
16. Structural performance of traveling wave antenna
Ch. XV. Single -Wire Traveling Wave Antenna (STA)
1. Diagram of the antenna and principle of its operation
2. Design formulas 567
3. Selection of antenna dimensiong 57
) .300
4. Electric parameters of the OB - 51
27-15
5. Electric parameters of the OB 100 5 8 1
25
Card 449M

Antennas (Cont. SOV 6112
6. Complex traveling wave antennas
7. Structural performance of the STA
CI-1. XVI. Antennas With Constant Beamwidt.h of the Directional
Pattern Within a Broad Wave Band. Antennas With
Logarithmic Periodic Structure. Other Possible Antenna
Types With Constant Bearnwidth Pattern
1. General remarks. Logarithmic periodic antennas -5 9 2
2. Circuit diagram and principle of logarithmic antenna operation 593
3. Results of experimental investigations on logarithmic antennas
with models F) 0 0
4. Use of logarithmic antennas for short waves 606
5. Other possible circuit diagrams of antenna directivity patterns
of constant width (114

,'IJ'1?1-10R:
'217'Lh":
IIERIODICAL:
S/108/62/017/011/003/007
D413/0308
Lokshin, V.L. and Yompollskiy, V.G.'
im ap?,roximation technique for calculating mutual
impedances of vil).rators
Ittadiotelthnika, v. 17, no. ll.- 1962, 23-29
Ta:XT: The precise formulas for the mutual impedance are
too complex for 'use in design calculations on multi-element arrays,
Ohile the published curves only cover a few of the cases needed in
practice. 'the authors !)resent a new appro~cimation to the general
formula, and compare the results from it with accurate.calculations
for various cases. The new fortnula appears to give food agreement
for the resistive componcnt of mutual impddance provided the Nd;bra dP_-1eS
tors are not much loiiger than full-wave and whatever the distance
,between them: the reactive component in not accurately given when
the separation is lessthan /1/2, since the basis of the approxima-
tion br6aks down, but a correction can be developed to take account
of this. There are 11 figures.
SUBMITTED: January 3, 1962 Card 1A

L 12814;-6 Sdr(l)/BDS/E~V-2 AFFTr,/A,-.D/AFfOg/ESD,.,3/,,~.PGC J_4/Fk-4
a_M:_~OFn- F
4 wit S/ir-9/63/003/004/604/03 0
AUTHOR: Yampollskib-i--G.
TITLE: -Diffraction of a-flat electromagnetic wave in a system of metal strips
PERIODICAL: Radiotelchritka ielektronika, v. 8., no. 4, 1963., 564-576
examines the -diffraction -of - a, flat electron, amotic; wav
TEXT. a in
a nornal fall upon a periodic grid consisting of parallel metal otrips. The re-
s
-its -of co=utations for a number of ind�vidual oa-aes, arc, given. He raportz th-at
u
a com L
parison of experimental results indicates that, in cases where grid density
'q is -the degree of diffraction in a periodic grid consisting of flat metal
low.,
strips is identical to thediffraction that would be obtained Vdth a grid consis
ing of round-seotion' -wires with a denzity of 0/20 The obvious conclusion is tha~t
grids made of round vireo reflect electromagnetic; waves much more intensively than
do systems of flat metal stripa. 7his charactox--intic., is retained Yrith 0 < 0.3
and 0.4.
SUBMITTEDs March 15, 1962.

S11 08/63/018/002/002/010
D413/D308
AUTHOR: Yampollsk~y, V. G., Member.of the Society (see Asso-
ciation)
TITLE: Th~ effect of phase distortion ot the efficiency of
an aperiodic antenna
PERIODI AL: Radiotekhnika, v. 18, no. 2, 1963, 10-14
TEXT., The author uses -the methods developed in his earlier paper
(Radiotekhnika, v. 10, 110-59 1955) to analyze -the direction of
--maximum radiation and the gain of an aperiodic antenna for the ge-
neral case of any distribution of field amplitude and phase over
the aperture. He gives design formulas and shows that they are
sufficiently accurate under certain phase conditions which are
readily satisfied with non-uniform illumination. He takes as a par-
ticular case a symmetrically illuminated aperture with-phaBe die-
approximated by a third-order polynomial and two alter-
native polynomial amplitude distribution8p derives the expressions
for,gain and direction of ipaximum and plote some of the calcula-
1/2

S11 08/63/018/002/002/010
The effect of phase D413/D308
ted values, a few of which have been compared with accurate values
obtained from Fresnel integrals and have shown satisfactory agree-
ment. There are 4 figures.
A880OIATION: Nauchno-tokhnichookoye obuhohoetvo radiotokhniki i
elektroavyazi im. A. 8. Popova (scientific and Tech'
nical Society of Radio Engineering and Electrical
Communications imeni A. S. Popov) Z-Abstracter's
note: Name of Association.taken from first page o:f
journall
SUBMITTED: April 26, 1961
Card 2/2.
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